|
Customer | Program Name | Hardware Description | Type | Launch |
JPL | IPEX II (Interferometer Program Experiment) | Nonretractable model for shuttle experiment | ADAM Mast | 1997, Shuttle |
JPL | SRTM (Shuttle Radar Topographic Mapper) | Radar Interferometry Antenna Support Boom | ADAM Mast | 1999, Shuttle |
MacDonell-Douglas | MODES (Middeck 0-g Dynamics Experiment Structural Test Model) | Articulated truss structure model for on-orbit astronaut experiments | Articulated mast | 1991 Shuttle |
MacDonell-Douglas | MODES II | Articulated truss structure for on-orbit experiments | Articulated mast | 1994, Shuttle |
Fairchild Space | EUVE (Extreme UltraViolet Explorer Platform) | High gain antenna extension and support | Coilable mast | 1992, Delta II |
GE Astro | UARS (Upper Atmosphere Research Satellite) | ZEPS instrument support and extend | Coilable mast | 1990, Shuttle |
JPL | Galileo Interplanetary Explorer | Double magnetometer masts with mid-length structure | Coilable mast | 1989 Shuttle |
JPL | Cassini | Interplanetary probe magnetometer mast | Coilable mast | 1997, Titan IV |
JPL | IMP (Imager for Mars Pathfinder) | Mars lander deployable camera mast | Coilable mast | 1997, Delta |
Lockheed | SAFE (Solar Array Flight Experiment) | Flexible solar array flight demonstration | Coilable mast | 1984 Shuttle |
Lockheed Martin | Lunar Prospector | Three Deployable Masts | Coilable mast | 1998, Athena |
Lockheed Martin | Carousel deployed mast | Classified | Coilable mast | Classified |
Lockheed Martin | EOS-AM (Terra) | Solar array deployment mast system | Coilable mast | 1999, Atlas II |
Martin Marietta | GGS (Global Geospace Science) WIND Spacecraft | Two Instrument Masts | Coilable mast | 1994, Delta II |
Martin Marietta | GGS (Global Geospace Science) POLAR Spacecraft | Two instrument masts | Coilable mast | 1996, Delta II |
Naval Research Laboratory | LACE (Low Energy Atmospheric Compensation Experiment) | Three 150-ft long coilable masts | Coilable mast | 1990, Delta II |
U. Mass Lowell | MIDEX IMAGE | Spin axis antenna deployment booms | Coilable mast | 1999 |
JPL | Galileo Interplanetary Explorer | RPM Thermal Control Structure | Cover | 1989 Shuttle |
JPL | Galileo Interplanetary Explorer | Plasma Wave Antenna | Dipole antenna | 1989 Shuttle |
 | Suborbital Antenna Boom | Dipole antennas | Dipole antenna | 1993, Black Brant |
Lockheed Martin | International Space Station Solar Array Mast-Canisters | FASTMast deployer for solar arrays | FASTMast | 1999-2002, Shuttle |
Martin Marietta | TSS (Tethered Satellite System) | Articulated mast satellite staging deployable structure. | FASTMast | 1992, Shuttle |
Martin Marietta | TSS - Reflight (Tethered Satellite System) | Articulated mast satellite staging deployable structure. | FASTMast | 1996, Shuttle |
Lockheed Martin | OTD (ORU Transfer Device) | Deployable Tubular Boom System | Nesting boom | 1997, Shuttle |
Lockheed Martin | A2100 Hinges and SADA’s | Manufacture and testing of Lockheed Martin design | Other | 1998 |
CTA Space Systems | INDOSTAR Solar Array | Rigid Substrate Solar Array | PUMA Solar Array | 1997, Ariane |
Orbital Sciences | BSAT -2 A | Rigid Substrate Solar Array | PUMA Solar Array | 2001 &2002 |
Orbital Sciences | NSTARc | Rigid Substrate Solar Array | PUMA Solar Array | 2002, Ariane |
Orbital Sciences | Galaxy XII | Rigid Substrate Solar Array | PUMA Solar Array | 2003, Ariane-5 |
Orbital Sciences | BSAT-2C | Rigid Substrate Solar Array | PUMA Solar Array | 2003, Ariane-5 |
Lockheed Martin | Space Station Freedom Solar Alpha Rotary Joint (PG-1) | Ten-ft rotary gimbal for sun tracking | Rotating joint | 2002, Shuttle |
BMDO/JPL | New Millennium Deep Space 1 | Next Generation Concentrator Solar Array | SCARLET solar array | 1998, Delta II |
RCA Astro | SOOS | Gravity gradient masts | Tubular boom | 1984-5, Scout |
U. Mass Lowell | MIDEX IMAGE | Dipole antennas | Wire Deployer | 1999 |
